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Reduced-order modelling of non-linear, transient aerodynamics of the HIRENASD wing

Published online by Cambridge University Press:  20 April 2016

K. Lindhorst ,
M.C. Haupt  and
P. Horst
K. Lindhorst*
Affiliation:
Institute of Aircraft Design and Lightweight Structures (IFL), Technische Universität Braunschweig, Hermann-Blenk-Straße, Braunschweig, Germany
M.C. Haupt
Affiliation:
Institute of Aircraft Design and Lightweight Structures (IFL), Technische Universität Braunschweig, Hermann-Blenk-Straße, Braunschweig, Germany
P. Horst
Affiliation:
Institute of Aircraft Design and Lightweight Structures (IFL), Technische Universität Braunschweig, Hermann-Blenk-Straße, Braunschweig, Germany
*
[email protected]
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Abstract

In this paper, a surrogate model approach for non-linear aerodynamics is presented in order to reduce the computational effort of coupled aeroelastic analyses. The usability of the approach is demonstrated in static as well as transient aeroelastic analyses of the HIRENASD wing-fuselage configuration. Furthermore, it is shown that the surrogate model approach is able to cover variations of flow conditions at a fixed Mach and Reynolds number.

Keywords

aeroelasticityreduced order modelingsurrogate modelingneural networksproper orthogonal decompositionHIRENASD
Type
Research Article
Information
The Aeronautical Journal , Volume 120 , Issue 1226 , April 2016 , pp. 601 - 626
Copyright
Copyright © Royal Aeronautical Society 2016 

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